Blocking/deblocking resin systems for use as a “co-cure-ply” in the fabrication of large-scale composite structure
Abstract
A method for bonding composite structures which includes providing a first and second composite substrate and coupling a co-cure prepreg tape having chemically protected polymerizable functional groups onto a surface of both the first and second composite substrates. The first and second composite substrates are then cured to the co-cure prepreg tape at a first temperature to form a co-cure prepreg tape portion where the first and second composite substrates are fully cured and the co-cure prepreg tape is partially cured. The co-cure prepreg tape portion of the first composite substrate is then coupled to the co-cure prepreg tape portion of the second composite substrate and a deprotection initiator is applied to facilitate deprotection of the chemically protected polymerizable functional groups and cure the co-cure prepreg tape portion of the first and second composite substrates to form a single covalently bonded composite structure.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1. A method for bonding composite substrates comprising:
providing a first composite substrate and a second composite substrate wherein both the first composite substrate and the second composite substrate are uncured or partially cured and comprise one or more reinforcement fibers and a first curable resin;
coupling a co-cure prepreg tape onto a faying surface of both the first and second composite substrates wherein the co-cure prepreg tape comprises a second curable resin having one or more chemically protected polymerizable functional groups;
curing the first and second composite substrates to the co-cure prepreg tape at a first temperature to form a co-cure prepreg tape portion wherein the first and second composite substrates are fully cured and the co-cure prepreg tape is partially cured;
coupling the co-cure prepreg tape portion of the first composite substrate to the co-cure prepreg tape portion of the second composite substrate;
applying a second temperature to facilitate deprotection with water and a hydrolysis catalyst of the chemically protected polymerizable functional groups to give unprotected polymerizable functional groups and cure the co-cure prepreg tape portion of the first composite substrate to the co-cure prepreg tape portion of the second composite substrate to form a single covalently bonded composite structure.
2. The method of claim 1 , further comprising
applying a reflow temperature to the co-cure prepreg tape coupled to the first and second composite substrates before curing at the first temperature.
3. The method of claim 1 , wherein:
the first temperature is from about 75° C. to about 250° C. and the second temperature is from about 75° C. to about 250° C.
4. The method of claim 1 , wherein:
the first curable resin comprises an epoxide and an amine.
5. The method of claim 1 , wherein:
the second curable resin comprises an epoxide and a chemically protected polymerizable amine.
6. The method of claim 1 , wherein:
the one or more chemically protected polymerizable functional groups is an aldimine.
7. The method of claim 1 , wherein:
the one or more chemically protected polymerizable functional groups is an ketimine.
8. The method of claim 1 , wherein:
the unprotected polymerizable functional groups are an amine.
9. The method of claim 8 , wherein:
the amine is 4,6-diethyl-2-methylbenzene-1,3-diamine.
10. The method of claim 1 , wherein:
the hydrolysis catalyst is selected from the group consisting of acidic alumina, imidazole, and combinations thereof.
11. A method for bonding composite substrates comprising:
providing a co-cure prepreg layer cured to a surface of both a first composite substrate and a second composite substrate wherein the co-cure prepreg layer comprises a chemically protected polymerizable functional group;
coupling a portion of the co-cure prepreg layer cured to the first composite substrate to a portion of the co-cure prepreg layer cured to the second composite substrate;
applying a deprotection initiator to deprotect the protected polymerizable functional group of the co-cure prepreg layers and to couple the co-cure prepreg layers of the first and second composite substrates, to form a single covalently bonded composite structure.
12. The method of claim 11 , wherein:
the deprotection initiator comprises a heat source, a chemical reagent, a light source, a mechanical force, or a combination thereof.
13. The method of claim 11 , wherein:
the first and second composite substrates comprise a curable resin material having an amine and an epoxide.
14. The method of claim 11 , wherein:
the first and second composite substrates comprise one or more reinforcement fibers.
15. The method of claim 1 , wherein:
the chemically protected polymerizable functional groups is an aldimine.
16. The method of claim 11 , wherein:
the chemically protected polymerizable functional groups is an ketimine.
17. The method of claim 11 , wherein:
the single covalently bonded composite structure comprises a crosslinked amine-cured epoxy polymer network.
18. A co-curable composite structure comprising:
a first and a second uncured or partially cured composite substrate comprising a first curable resin wherein the first curable resin comprises a first epoxide and an amine;
a first co-cure prepreg layer coupled to a surface of the first uncured or partially cured composite substrate and a second co-cure prepreg layer coupled to a surface of the second uncured or partially cured composite substrate wherein the first and the second co-cure prepreg layers comprises a second curable resin having a second epoxide and a chemically protected amine;
wherein the first and the second uncured or partially cured composite substrate and the first and the second co-cure prepreg layers are cured together at a first temperature until the amines of the first and the second uncured or partially cured composite substrate are functionally fully cured; wherein the first co-cure prepreg layer of the first composite substrate is coupled to the second co-cure prepreg layer of the second composite substrate to form the co-curable composite structure; and
wherein the chemically protected amine of the first and the second co-cure prepreg layers are partially cured and remains latent until an additional deprotection and co-cure step.
19. The co-curable composite structure of claim 18 , wherein:
the chemically protected amine is an aldimine.
20. The co-curable composite structure of claim 18 , wherein:
the chemically protected amine is a ketimine.Cited by (0)
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